Hybrid airfoil design method to simulate full-scale ice accretion throughout a given α range

Journal of Aircraft

Volumn 35, Issue 2, 1998, Pages 233-239

  Saeed, Farooq ^a,b   Selig, Michael S ^a,b   Bragg, Michael B ^a,b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DROP FORMATION; ICE; VISCOUS FLOW;

ALPHA RANGE; ANGLE OF ATTACK; HYBRID AIRFOILS; ICE ACCRETION;

AIRFOILS;

EID: 0032026779     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2289     Document Type: Article

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